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A B C D E F G H I J K L M N O P Q R S T U V W X Y Z ALL

A

  • Abbasi, Hossein Reza Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]

  • Aghalari, Alireza Designing and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]

  • Ajorkar, Abbas Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]

  • Alavi pour, Mojtaba Optimal Trajectory Design of an Upper Stage for Satellite Injection into Geostationary Orbit Using Limited Thrust [Volume 9, Issue 4, 2017, Pages 13-25]

  • Alisadesghi, hamed Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]

  • Amiri, Shervin Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]

  • Amiri Atashgah, MohammadAli Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]

  • Arefkhani, Hamed Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]

  • Arefkhani, Hamed Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]

  • Arvan, Mohammad Reza Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2017, Pages 39-50]

  • Asadi golzar, Mohammad The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

D

  • Daneshjoo, Kamran Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]

  • Dehghan, Seyed Mohammad Mehdi Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]

  • Dehghan, Seyed Mohammad Mehdi Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]

  • Dehghani Mohammad-Abadi, Mohsen Approximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]

E

  • Esmaeilzadeh, Seyed Majid (Technical Note) Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]

F

  • Fani Saberi, Farhad Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]

  • Fani Saberi, Farhad Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]

  • Farhang Laleh, Farhad Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]

  • Fazlyab, Alireza Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]

  • Fiuzy, Mohammad (Technical Note) Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]

G

  • Gazerpour, Hamid Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]

  • Ghahramani, Mohammad Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]

  • Golro, Ali Akbar Role of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2017, Pages 27-37]

H

  • Hajebrahimi, Zahra The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Hashemi, Malihe (Technical Note) Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]

  • Hashemi Mehne, Seyed Hamed Review of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector [Volume 9, Issue 1, 2016, Pages 73-89]

J

  • Jalali Naini, Seyed Hamid Approximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]

K

  • Kabganian, Mansor Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]

  • Kalhor, Ahmad A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]

  • Karimi, Hasan Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]

  • Kazemi, Ali The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Kazemi, H. Role of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2017, Pages 27-37]

  • Khaledi, Neda The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Khodadadiyan, Sajad Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]

  • Kosari, Amirreza A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]

  • Kosari, AmirReza Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]

M

  • Madadkar, Abdollah A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]

  • Mahmoud-Aghdami, Ashkan Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]

  • Mansori-Nezhad, Hosein Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]

  • Mehdi-Abadi, Mehran Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]

  • Mehrabi, Ali Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 59-72]

  • Mirshams, Mehran Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]

  • Mohammadi, Leyla Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]

  • Mohammadkhani, Gholamreza Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]

  • Mohammadzaman, Iman Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2017, Pages 39-50]

  • Mortazavi, Mehdi Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]

  • Mortazavi-Bek, Mehdi Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]

  • Mosavi Mashhadi, Seyed Kamaleddin (Technical Note) Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]

  • Mosvi, Seyed Mohammad Sadegh Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]

N

  • Naderifar, Javad Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]

  • Naghash, Abolghasem Determining orbital element on Earth Observation Repeat-Ground-Track orbit [Volume 9, Issue 2, 2016, Pages 77-83]

  • Naseh, Hasan Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]

  • Naseh, Hasan Space Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2017, Pages 1-12]

  • Nikbakht, Vahid The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Nikkhah, Amir Ali Optimal Trajectory Design of an Upper Stage for Satellite Injection into Geostationary Orbit Using Limited Thrust [Volume 9, Issue 4, 2017, Pages 13-25]

O

  • Ommi, Fathallah Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 59-72]

R

  • Ramesh, Davood Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]

  • Ramezani-Najafi, Hamed Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]

  • Roghangir, seyed Amirreza Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]

  • Roshanian, Jafar Optimal Trajectory Design of an Upper Stage for Satellite Injection into Geostationary Orbit Using Limited Thrust [Volume 9, Issue 4, 2017, Pages 13-25]

S

  • Sabahi, Mohammad Farzan Using the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]

  • Saberali, Sayed Mohamad Using the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]

  • Sadeghi, Ahmad Reza Using the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]

  • Saghari, Asad Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]

  • Salem, Javad Reduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2017, Pages 51-63]

  • Samadi Khoshkho, Zahra Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]

  • Shahravi, Majid Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]

T

  • Tavakoli, Amir Hossein Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]

  • Tayebi, Javad Designing and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]

  • Torabi, Payman Determining orbital element on Earth Observation Repeat-Ground-Track orbit [Volume 9, Issue 2, 2016, Pages 77-83]

V

  • Veysi, Hadi Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]

Y

  • Ya’ghob-nezhad, Saeedeh Review of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector [Volume 9, Issue 1, 2016, Pages 73-89]

  • Yavari, Reza Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2017, Pages 39-50]